What was found
FUSELAGE FRAME AT FS 438.25 LT HAD CHAFFING. REPAIRED IAW ACFT ENGINEERING REPORT NR 6772-2 REV 1R.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE FRAME AT FS 438.25 LT HAD CHAFFING. REPAIRED IAW ACFT ENGINEERING REPORT NR 6772-2 REV 1R.